An improved transverse shear deformation theory for laminated anisotropic plates /

Stress-concentration factors for finite orthotropic laminates with a pin-loaded hole /

Crews, John H.
Raju, I. S.
Hong, C. S.
Joint Institute for Advancement of Flight Sciences.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"May 1981"--Cover."The George Washington University Joint Institute for Advancement of Flight Scienc...

Wave surfaces due to impact on anisotropic fiber composite plates /

Moon, F. C., 1939-
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1971

Prepared at Lewis Research Center."September 1971."N 71-33672.Includes bibliographical references (p...

A theory of anisotropic viscoelastic sandwich shells /

Baylor, John L.
United States. National Aeronautics and Space Administration.
University of California, Berkeley.

January 1966

"Prepared under Grant No. NsG-637 by University of California, Berkeley, Calif. for National Aeronau...

Shear-flexible finite-element models of laminated composite plates and shells /

Noor, Ahmed Khairy, 1938-
Mathers, Michael D. (Michael Douglas)
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 42-45).Mode ...

Buckling behavior of long symmetrically laminated plates subjected to combined loadings /

Nemeth, Michael P.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 11-12).Mode of access: I...

A review of refined shear deformation theories of isotropic and anisotropic laminated plates

GHUGAL, YM
SHIMPI, RP

January 2002

A review of displacement and stress based refined theories for isotropic and anisotropic laminated p...

An approximate buckling analysis for rectangular orthotropic plates with centrally located cutouts /

Nemeth, Michael P.
Johnson, Eric R.
Stein, Manuel.
Langley Research Center.

January 1986

Prepared at Langley Research Center."February 1986"--Cover.Includes bibliographical references (p. 9...

New triangular and quadrilateral plate-bending finite elements /

Narayanaswami, R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 61).Mode of ...

Postbuckling response of long thick isotropic plates loaded in compression including higher order transverse shearing effects /

Stein, Manuel.
Sydow, P. Daniel.
Librescu, Liviu
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 13.Mode of access: Internet

Theoretical study of corrugated plates : shearing of a trapezoidally corrugated plate with through lines permitted to curve /

Lin, Chuan-jui.
Libove, Charles.
United States. National Aeronautical and Space Administration.
Syracuse University.
Langley Research Center.

January 1971

"Prepared by Syracuse University ... for Langley Research Center."N72-13881.Cover title.Includes bib...

Numerical analysis and parametric studies of the buckling of composite orthotropic compression and shear panels /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 67-68).Mode ...

A review of refined shear deformation theories of isotropic and anisotropic laminated plates

Y. M. Ghugal
R. P. Shimpi

January 2002

ABSTRACT: A review of displacement and stress based refined theories for isotropic and anisotropic l...

A new look at numerical analyses of free-edge stresses in composite laminates /

Raju, I. S.
Goree, J. G.
Whitcomb, J. D.
Langley Research Center.
Joint Institute for Advancement of Flight Sciences.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center.""The George Washington University, Joint Institute for Advanceme...

Buckling analysis for axially compressed flat plates, structural sections, and stiffened plates reinforced with laminated composites /

Viswanathan, A. V.
Miller, R. E., Jr.
Soong, Tsai-Chen.
Langley Research Center.
Boeing Company.

January 1971

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Includes bibliographica...

Tensile stress-strain behavior of graphite/epoxy laminates /

Garber, D. P. (Donald P.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Kentron Technical Center.
Langley Research Center.

January 1982

"Kentron Technical Center.""August 1982"--Cover.Includes bibliographical references.Mode of access: ...

Stress-concentration factors for finite orthotropic laminates with a pin-loaded hole /

Crews, John H.
Raju, I. S.
Hong, C. S.
Joint Institute for Advancement of Flight Sciences.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"May 1981"--Cover."The George Washington University Joint Institute for Advancement of Flight Scienc...

Wave surfaces due to impact on anisotropic fiber composite plates /

Moon, F. C., 1939-
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1971

Prepared at Lewis Research Center."September 1971."N 71-33672.Includes bibliographical references (p...

A theory of anisotropic viscoelastic sandwich shells /

Baylor, John L.
United States. National Aeronautics and Space Administration.
University of California, Berkeley.

January 1966

"Prepared under Grant No. NsG-637 by University of California, Berkeley, Calif. for National Aeronau...

Shear-flexible finite-element models of laminated composite plates and shells /

Noor, Ahmed Khairy, 1938-
Mathers, Michael D. (Michael Douglas)
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 42-45).Mode ...

Buckling behavior of long symmetrically laminated plates subjected to combined loadings /

Nemeth, Michael P.
Langley Research Center.

January 1992

Prepared at Langley Research Center.Includes bibliographical references (p. 11-12).Mode of access: I...

A review of refined shear deformation theories of isotropic and anisotropic laminated plates

GHUGAL, YM
SHIMPI, RP

January 2002

A review of displacement and stress based refined theories for isotropic and anisotropic laminated p...

An approximate buckling analysis for rectangular orthotropic plates with centrally located cutouts /

Nemeth, Michael P.
Johnson, Eric R.
Stein, Manuel.
Langley Research Center.

January 1986

Prepared at Langley Research Center."February 1986"--Cover.Includes bibliographical references (p. 9...

New triangular and quadrilateral plate-bending finite elements /

Narayanaswami, R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 61).Mode of ...

Postbuckling response of long thick isotropic plates loaded in compression including higher order transverse shearing effects /

Stein, Manuel.
Sydow, P. Daniel.
Librescu, Liviu
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 13.Mode of access: Internet

Theoretical study of corrugated plates : shearing of a trapezoidally corrugated plate with through lines permitted to curve /

Lin, Chuan-jui.
Libove, Charles.
United States. National Aeronautical and Space Administration.
Syracuse University.
Langley Research Center.

January 1971

"Prepared by Syracuse University ... for Langley Research Center."N72-13881.Cover title.Includes bib...

Numerical analysis and parametric studies of the buckling of composite orthotropic compression and shear panels /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 67-68).Mode ...

A review of refined shear deformation theories of isotropic and anisotropic laminated plates

Y. M. Ghugal
R. P. Shimpi

January 2002

ABSTRACT: A review of displacement and stress based refined theories for isotropic and anisotropic l...

A new look at numerical analyses of free-edge stresses in composite laminates /

Raju, I. S.
Goree, J. G.
Whitcomb, J. D.
Langley Research Center.
Joint Institute for Advancement of Flight Sciences.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center.""The George Washington University, Joint Institute for Advanceme...

Buckling analysis for axially compressed flat plates, structural sections, and stiffened plates reinforced with laminated composites /

Viswanathan, A. V.
Miller, R. E., Jr.
Soong, Tsai-Chen.
Langley Research Center.
Boeing Company.

January 1971

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Includes bibliographica...

Tensile stress-strain behavior of graphite/epoxy laminates /

Garber, D. P. (Donald P.)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Kentron Technical Center.
Langley Research Center.

January 1982

"Kentron Technical Center.""August 1982"--Cover.Includes bibliographical references.Mode of access: ...

Stress-concentration factors for finite orthotropic laminates with a pin-loaded hole /

Crews, John H.
Raju, I. S.
Hong, C. S.
Joint Institute for Advancement of Flight Sciences.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"May 1981"--Cover."The George Washington University Joint Institute for Advancement of Flight Scienc...

Wave surfaces due to impact on anisotropic fiber composite plates /

Moon, F. C., 1939-
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1971

Prepared at Lewis Research Center."September 1971."N 71-33672.Includes bibliographical references (p...

A theory of anisotropic viscoelastic sandwich shells /

Baylor, John L.
United States. National Aeronautics and Space Administration.
University of California, Berkeley.

January 1966

"Prepared under Grant No. NsG-637 by University of California, Berkeley, Calif. for National Aeronau...

An improved transverse shear deformation theory for laminated anisotropic plates /

Abstract

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An improved transverse shear deformation theory for laminated anisotropic plates /

Abstract

Extracted data

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